Mixing method

Description

[0001] This invention relates generally to a mixing method in a mixing machines of the batch type, that is, machines having a mixing chamber so shaped to accommodate two counter-rotating winged rotors that mix batches of ingredients fed successively to the mixing chamber from a charging chamber by a reciprocating ram. Once mixed the ingredients are removed through a discharge opening and a door closes the opening for mixing a further batch in the chamber.

[0002] The present invention seeks to optimize the behavior of the ingredients being mixed by providing a cyclically repeatable window of interaction between the winged rotors as they turn in opposite directions through at least one revolution of the rotors.

[0003] Conventional high intensity batch mixers have two counter-rotating winged rotors, driven at the same or slightly different speeds through connecting gears, and the winged rotors act on the ingredients to move the material from one portion of the mixing chamber to another. The rotor wings also act on the ingredients to achieve movement of the material along the axis of each of the rotors. Prior art US-A-3,610,585 illustrates a typical prior art rotor configuration, it will be noted that these rotors have blades or wings which do not intermesh with one another so that these rotors can be driven at either slightly different speeds or at the same speed.

[0004] The general object of the present invention is to optimize the mixing behaviours of the mixer by providing a cyclically repeatable flow pattern in the window of interaction between the rotors in the mixing chamber where the opposed rotors and wings interact with one another.

[0005] According to the present invention, there is provided a method of mixing a batch of ingredients in a mixing machine of the batch type having a housing defining two horizontally opposed parti-cylindrical cavities with open sides facing one another and defining a chamber, said housing having vertically spaced inlet and outlet openings communicating with said chamber and with said cavities, axially opposed end walls for said cavities and chamber, a ram for closing said inlet opening, a door for closing said outlet opening, two opposed, non-intermeshing mixing rotors respective ones of said rotors being provided in respective ones of said cavities, each said rotor having at least two generally helical shaped wings each wing having a leading end and a trailing end, said method of mixing comprising the steps of:
   solely driving said rotors at identical speed in opposite directions on parallel horizontal axes,
   orienting said rotors at a predetermined rotational alignment relationship between them,
   said predetermined rotational alignment being within ± 20 degrees of zero degree alignment of the leading ends of the first rotor wings,
   locating a first of said rotor wings on each rotor for serving as a first pair of opposed rotor wings, moving said first pair of opposed rotor wings at identical rotor speed through a horizontal reference rectangle defined by said rotor axes and said two end walls, said first pair of opposed rotor wings moving through said rectangle on opposite sides of a first diagonal of said rectangle with said leading ends of said first pair of opposed rotor wings being adjacent respectively to the end walls and moving through said rectangle at substantially the same first time for transversely and axially squeeze mixing the ingredients between said first pair of opposed rotor wings,
   said transversely and axially squeeze mixing between said first pair of opposed rotor wings being toward said first diagonal from opposite sides of said first diagonal,
   locating a second of said rotor wings on each rotor for serving as a second pair of opposed rotor wings, said second pair of opposed rotor wings moving through said rectangle on opposite sides of a second diagonal of said rectangle with said leading ends of said second pair of opposed rotor wings being adjacent respectively to the end walls and moving through said rectangle at substantially the same second time,
   said second time being at a point in time after said first pair of opposed rotor wings have passed through said rectangle for transversely and axially squeeze mixing the ingredients between said second pair of opposed rotor wings moving through said rectangle, and
   said transversely and axially squeeze mixing between said second pair of opposed rotor wings being toward said second diagonal from opposite sides of said second diagonal,
   thereby said transversely and axially squeese mixing from opposite sides of said first diagonal and from opposite sides of said second diagonal are each repeated during each and every revolution of the two rotors.

[0006] In its presently preferred form the mixing machine of the method of the present invention includes a housing defining a mixing chamber, and more particularly defining horizontally opposed parti-cylindrical cavities with open sides facing one another. The mixing chamber is further defined by the lower end of the ram that feeds the materials into the chamber through an inlet opening, and by a hinged door that closes a lower outlet opening. The ram and door cooperate with these chamber cavities to define the mixing chamber. Counter-rotating rotors are provided in each of the parti-cylindrical cavities and each rotor has at least two generally spiral shaped wings, each wing having a leading end and a trailing end. The rotors turn on parallel axes and these axes cooperate with the end walls of the mixing chamber to define a rectangle in a horizontal reference plane extending across the cavities and mixing chamber. A window of variable geometry is provided between these rotors in the reference plane as a result of the rotor wings moving through said plane. Each rotor wing is arranged so that its leading end is located adjacent one of the end walls of the mixing chamber and so that its trailing end is provided intermediate the end walls and in spaced circumaxial relationship behind the leading end by an angle alpha. Furthermore, the wings are more particularly provided on opposed rotors in opposed pairs, one pair provided on opposite sides of one diagonal of the rectangle and a second pair of rotor wings provided on opposite sides of the second diagonal of the rectangle. Thus, the leading ends of these paired wings will preferably move simultaneously through the reference plane in pairs, and at predetermined times during the cycle of revolution for the rotors themselves so that the successively formed window shapes and sizes are repeatable during every revolution of the rotors. In its presently preferred form the mixing machine is provided with four pairs of rotor wings each of which pairs acts to so form the variable geometry window during each 90 degrees of rotation of the winged rotors.

[0007] At least one winged pair comprises long wings that overlap one another axially in cooperating to so define the window, and in the presently preferred embodiment two such pairs of long wings are provided to act on the mix in a cyclical fashion that repeats not only every 360 degrees or each revolution of the rotors but also repeats itself during each 180 degrees of travel for these rotors.

[0008] Figure 1 is a schematic view illustrating the overall mixing machine in vertical section.

[0009] Figure 2 is a vertical section through the lower portion of the machine illustrated in Figure 1, and shows the ram in its down position.

[0010] Figure 3 is a horizontal section taken generally on the line 3-3 of Figure 1.

[0011] Figure 3A is a schematic view of the relationship between the two counter-rotating rotors in the preferred alignment pursuant to the present invention.

[0012] Figure 4 is a view similar to Figure 3A but taken at a slightly later instant of time wherein both rotors have turned through 90 degrees relative to the position illustrated in Figure 3A.

[0013] Figure 5 is a view similar to Figures 3A and 4, but illustrating the rotors after a further 90 degrees of rotation, that is after having rotated 180 degrees from the Figure 3A positions.

[0014] Figure 6 illustrates in schematic fashion, the orientation of the rotor wings in the views of Figures 3A by unwrapping the cylindrical envelope which contains the rotor wings.

[0015] Figure 7 is a view similar to Figure 6 but illustrating the rotor wing orientations after 90 degrees of rotation for the rotors, and corresponds to Figure 4.

[0016] Figure 8 is a view similar to Figures 6 and 7 but illustrating the rotor wings 90 degrees beyond the position of Figure 7 and 180 degrees beyond the position of Figure 6, and corresponds to Figure 5.

[0017] Figure 9 is a graphical presentation of the effect on rotor productivity (Kg/hr) of departing slightly from 0° alignment of the rotors, that is with one rotor provided in a different angular relationship from the zero degree relationship suggested in Figures 3A, 4 and 5.

[0018] Figure 10 is a graphical presentation of the effect on mix viscosity of slight non-alignment between the rotors as suggested in Figure 9, both Figure 9 and 10 having the same horizontal units of rotor rotational alignment (that is, 0° alignment +/- non-alignment).

[0019] Turning now to the drawings in greater detail, Figures 1 and 2 show a mixing machine including a vertically reciprocable ram 10 movable between the position shown in Figure 1 and the position shown in Figure 2 to move a batch of ingredients to be mixed from a charging chamber 11 into a mixing chamber 17. Two counter-rotating rotors 13 and 13a have wings that act on these ingredients to achieve a thorough mixing thereof. The reader is referred to previously mentioned prior US-A-3,610,585 and to US-A-2,962,186, issued November 29, 1960 to C.F. Gottschalk, for a more complete description of the general aspects of such a mixing machine.

[0020] The ingredients are initially introduced to hopper 15 while the ram 10 is in its raised position (Figure 1) so that the ingredients drop downwardly into the chamber 11 where they are compressed and fed into the mixing chamber 17 by the ram 10. Once a batch has been mixed a hinged door 14 opposite the ram 10 is opened to withdraw the mixed materials. A locking device 25 is provided for securing the door 14 in place during mixing process. The ram 10 is preferably operated by a vertically reciprocable fluid motor in the form of actuator 16 having a piston 18 provided in a cylinder for movement of actuating rod 20. The ram 10 is attached to the lower end of actuating rod 20 externally of cylinder 16 and air pressure is selectively provided to line 22 for urging the piston downwardly from the Figure 1 position to the Figure 2 position. The ram 10 is retracted by air pressure to the opposite side of piston 18.

[0021] As best shown in Figure 3, rotors 13 and 13a are driven in opposite directions by a conventional gear mechanism 24 through drive motor 26. The gear mechanism 24 may comprise identical gears where the rotors are to be driven at the same speed, or in the alternative, a typical mixer generally has so-called friction ratio gears that permit the rotors to be driven at different speeds. However, and in accordance with the present invention, the gear mechanism 24 serves solely to drive the rotors 13 and 13a at the same speed and at opposite directions so as to realize the advantages of the present invention. Drive motor 26 may be of conventional configuration, and preferably includes suitable means for varying the speed of rotation for the rotors, said speeds being dictated in large part by the ingredients being mixed.

[0022] In accordance with the present invention non-intermeshing rotors 13 and 13a are driven in opposite directions as indicated by the arrows 28 and 28a, respectively in Figure 3A, such that diagonally opposed long wings 32 and 32a are arranged in opposed pairs to act on the mix in the window defined by the horizontal plane of the rotor axes 30 and 30a.

[0023] Although generally spiral shaped rotor wings of long and of short axial configuration are known from the prior art, and clearly shown in the aforementioned U.S.-A-3,610,585 for example, the present invention deals specifically with the phase relationship between the opposed rotors and the orientation of these spiral shaped wings such that in both rotors of Figure 3A the leading end 34 and 34a of each wing 32 and 32a, respectively, moves adjacent to one of the axially opposed end walls 36 and 38 of the mixing chamber.

[0024] As a result first of orienting the wings so that each has its leading end moving simultaneously through the reference plane defined by the rotor axes, and also as a result of orienting the wings so that their respective leading ends are located adjacent the end walls of the mixing chamber, the improved mixing is achieved in that the wings not only achieve a transverse or extensive mixing whereby the ingredients are urged from one parti-cylindrical cavity portion of the mixing chamber to the other, but intensified mixing is achieved as a result of squeezing of the mix axially toward the center of the mixing chamber 40 (where the center 40 is defined by the intersection between two diagonals 42 and 44 of a rectangle defined by the end walls 36 and 38 and by the rotor axes 30 and 30a). One such diagonal 42 has the paired rotor wings 32 and 32a provided on opposite sides thereof in Figure 3A, that is in a position for the rotors referred to hereinafter as a reference or zero degree position. The combination of transverse and axial squeeze mixing is illustrated in Figure 3A by the four force diagrams illustrating the tendency for the rotor wings 32 and 32a to achieve movement of the mix generally toward the one diagonal 42 defined above. Also, material at the center of the mixer is moved by the wings into the parti-cylindrical cavities to be mixed by a shearing action.

[0025] In further accordance with the present invention, a second pair of rotor wings 52 and 52a in each of the rotors 13 and 13a, respectively, are provided with their leading ends located in an axial plane defined by the trailing ends of the one pair of rotors 32 and 32a referred to previously. More particularly, this second pair of rotor wings 52 and 52a are provided at least 90 degrees behind the one longer pair referred to in the preceding paragraphs. These shorter rotor wings 52 and 52a act on the mix in substantially the same manner as the longer wings 32 and 32a described above. Each of these shorter wings 52 and 52a has its leading end adapted to simultaneously intersect the reference plane defined by the axes 30 and 30a at a point in time when the longer rotor wings 32 and 32a have passed through the reference plane and this next portion of the rotor cycle is illustrated in Figure 4. Note that these shorter rotor wings 52 and 52a are oriented on opposite sides of the second diagonal 44 referred to previously with reference to Figure 3A. Similar diagrams are also provided in Figure 4 to illustrate the fact that the mix is acted on by the wings so as to impart both transverse and axial flow directions whereby transverse and intensive mixing are achieved.

[0026] Figures 3A, 4 and 5 represent positions for the horizontally opposed rotors and more particularly of the rotor wings at 90 degree intervals during a portion of the 360 degrees of rotation for these rotors. The cycle of rotor rotation is repeated for each revolution of the rotors. In the preferred form of rotor illustrated in these views, that is where two pairs of long and two pairs of short rotor wings are provided thereon, it will be apparent that this cycle of window geometry defined by the wings and the body portions of the rotors in the area of the horizontal reference plane will repeat itself twice during each such rotor revolution cycle. For example, Figure 5 illustrates the configuration for the rotors 13 and 13a after 180 degrees of rotor rotation and, although Figure 5 is identical to Figure 3A, it is noted that the longer rotor wings 62 and 62a occupy the same positions as did the long one pair rotor wings and 32 and 32a in Figure 3A.

[0027] The repetitive window geometry between the opposed rotors achieved by the rotor wing configuration of the present invention is illustrated graphically in Figures 6, 7 and 8. The various frames illustrated in these views correspond to the rotor positions illustrated 3A, 4 and 5 and such frames are appropriately annotated in Figures 6, 7 and 8 for clarity. In Figure 6 the two adjacent frames illustrated at 35 and 35a on opposite sides of the mixer center line 39 shows schematically the long rotor wings 32 and 32a arranged at opposite sides of the diagonal 42. The adjacent frames are to illustrate the configuration for the other wings 52 and 52a discussed previously with reference to Figure 4 and 62 and 62a discussed above with reference to Figure 5.

[0028] Figure 7 simply shows the frames 35 and 35a having moved away from the center window defined by the opposed rotors and instead said window having been defined by the rotor wings 52 and 52a arranged at opposite sides of the second diagonal 44 as referred to previously.

[0029] Figure 8 illustrates another successive 90 degrees of rotation from that of Figure 7 wherein the center frames define the variable geometry window as a result of downward movement for the rotor wings 62 and 62a. Thus, Figure 6 corresponds to Figure 3A, Figure 7 to Figure 4, and Figure 8 to Figure 5 in terms of the orientation for the rotors 13 and 13a and more particularly of these wings in these various views.

[0030] Figures 9 and 10 must be interpreted together, and these graphical presentations illustrate qualitatively the results achieved by aligning the rotors as described above and rotating them at the same speeds to provide the cylindircally repeatable window geometry in the mixing chamber.

[0031] Figures 9 and 10 show the level of productivity and the viscosity level achieved with the rotors turning at different speeds relative to one another (more particularly, with a friction ratio of 1.12 to 1).

[0032] In figure 9 it will be seen that the productivity (kg/hr) is slightly better with the rotors aligned (zero degree), per the preferred arrangement described above, than with the random alignment that results from rotating one rotor at a speed different from that of the other rotor. In fact, one can achieve even greater "productivity" gains if the rotors are rotated at the same speeds and are aligned at a differential angular relationship than the zero degree alignment. However, "productivity" is not the sole criteria, and one must also consider viscosity since the purpose here is not simply to move material, as in a pump, but to mix material and provide material of minimum viscosity.

[0033] Figure 10 shows that the reduction in viscosity(at zero degree rotor alignment)is best.The combined results of tests for both viscosity and productivity show that the advantages of the present invention can be realized if only the rotors are close to the zero degree alignment referred to above. More specifically, the rotors should be within their +/- 20 degrees of this zero degree orientation for best results.

[0034] In conclusion then, the rotor configuration and operation as described above has led to improved viscosity and productivity for non-intermeshing synchronized rotors over the results one can expect from the non-synchronized rotors. The mix is rendered less viscous in a shorter period of time utilizing the above described rotor configurations as compared to the result achieved with the rotor configuration of prior art U.S.-A-3,610,585 for example.

Claims

1. A method of mixing a batch of ingredients in a mixing machine of the batch type having a housing defining two horizontally opposed parti-cylindrical cavities with open sides facing one another and defining a chamber(17), said housing having vertically spaced inlet and outlet openings (11,14) communicating with said chamber and with said cavities, axially opposed end walls (36,38) for said cavities and chamber, a ram (10) for closing said inlet opening, a door (14) for closing said outlet opening, two opposed,
non-intermeshing mixing rotors (13,13a), respective ones of said rotors being provided in respective ones of said cavities, each said rotor having at least two generally helical shaped wings (32,32a and 52,52a) each wing having a leading end (34, 34a) and a trailing end each trailing end being spaced circumaxially behind its leading end by an angle (a) relative to the direction of rotor rotation, said method of mixing comprising the steps of:
   solely driving said rotors at identical speed in opposite directions on parallel horizontal axes (30,30a),
   orienting said rotors at a predetermined rotational alignment relationship between them,
   said predetermined rotational alignment being within ± 20 degrees of zero degree alignment of the leading ends of the first rotor wings,
   locating a first of said rotor wings on each rotor for serving as a first pair of opposed rotor wings (32, 32a), moving said first pair of opposed rotor wings at identical rotor speed through a horizontal reference rectangle defined by said rotor axes and said two end walls, said first pair of opposed rotor wings moving through said rectangle on opposite sides of a first diagonal (42) of said rectangle with said leading ends of said first pair of opposed rotor wings being adjacent respectively to the end walls and moving through said rectangle at substantially the same first time for transversely and axially squeeze mixing the ingredients between said first pair of opposed rotor wings,
   said transversely and axially squeeze mixing between said first pair of opposed rotor wings being toward said first diagonal from opposite sides of said first diagonal,
   locating a second of said rotor wings (52,52a) on each rotor for serving as a second pair of opposed rotor wings, said first and second pair of rotor wings having their respective leading ends oriented in staggered angular relationship relative to one another said second pair of opposed rotor wings moving through said rectangle on opposite sides of a second diagonal (44) of said rectangle with said leading ends of said second pair of opposed rotor wings being adjacent respectively to the end walls and moving through said rectangle at substantially the same second time,
   said second time being at a point in time after said first pair of opposed rotor wings have passed through said rectangle for transversely and axially squeeze mixing the ingredients between said second pair of opposed rotor wings moving through said rectangle, and
   said transversely and axially squeeze mixing between said second pair of opposed rotor wings being toward said second diagonal from opposite sides of said second diagonal,
   thereby said transversely and axially squeese mixing from opposite sides of said first diagonal and from opposite sides of said second diagonal are each repeated during each and every revolution of the two rotors.

2. A method of mixing as claimed in claim 1, comprising the further steps of:
   locating a third and a fourth helical shaped wing on each rotor each wing having a leading and a trailing end, with said third wing on each rotor being opposite the first wing on the rotor and with the fourth wing on each rotor being opposite the second wing on the rotor,
   said third wings on the rotors for serving as a third pair (62,62a) of opposed rotor wings moving through the rectangle at identical rotor speed on opposite sides of said first diagonal with their leading ends being adjacent respectively to the end walls and moving through said rectangle at approximately a same third time when each of said rotors has turned 180 degrees from its respective position at said first time for transversely and axially squeeze mixing the ingredients between said third pair of opposed sides of said first diagonal,
   said transversely and axially squeeze mixing between said third pair of opposed rotor wings being toward said first diagonal from opposite sides of said first diagonal,
   said fourth wings on the rotors for serving as a fourth pair of opposed rotor wings moving through the rectangle at identical rotor speed on opposite sides of said second diagonal with their leading ends being adjacent respectively to the end walls and moving through said rectangle at approximately a same fourth time for axially and transversely squeeze mixing the ingredients between said fourth pair of opposed rotor wings moving through said rectangle on opposite sides of said second diagonal,
   said transversely and axially squeeze mixing between said fourth pair of opposed rotor wings being toward said second diagonal from opposite sides of said second diagonal,
   thereby said transversley and axially squeeze mixing from opposite sides of said first diagonal and from opposite sides of said second diagonal are each repeated twice during each and every revolution of the two rotors.

3. A method as claimed in claim 1, wherein said first pair of opposed rotor wings (32,32a) have sufficient length in the axial direction so that said wings of said first pair overlap one another axially.

4. A method as claimed in claim 1, wherein said second pair of opposed rotor wings (52,52a) have an axial length shorter than said first pair of opposed rotor wings.

5. A method as claimed in claim 1, wherein said angle (a) between the leading and trailing ends of each said wings of said first pair is at least 90 degrees.

6. A method as claimed in claim 2, wherein said second and fourth pairs of opposed rotors wings have their respective leading ends oriented in diametrically opposed relationship to one another, and wherein said first and third pairs of opposed rotor wings have their respective leading ends oriented in diametrically opposed relationship to one another, said diametrical opposed orientation of said paired leading ends being arranged at right angles to one another.

Ansprüche

1. Verfahren zum Mischen einer Charge von Mischungsbestandteilen in einer Mischmaschine des Chargentyps, mit einem Gehäuse, das zwei horizontal angeordnete, einander gegenüberliegende teilzylindrische Hohlräume mit einander gegenüberliegenden offenen Seitenflächen aufweist, wodurch eine Kammer (17) gebildet ist, wobei dieses Gehäuse voneinander vertikal beabstandete Einlaß- und Auslaßöffnungen (11, 14) aufweist, die in Verbindung mit dieser Kammer und mit diesen Hohlräumen stehen, einander axial gegenüberliegenden Endwänden (36, 38) für diese Hohlräume und diese Kammer, einen Stößel (10), um diese Einlaßöffnung abzuschließen, einer Klappe (14), um diese Auslaßöffnung abzuschließen, zwei einander gegenüberliegende,
nicht miteinander kämmende Mischrotoren (13, 13a), wobei jeder dieser Rotoren in einem der entsprechenden Hohlräume angeordnet ist, wobei jeder dieser Rotoren zumindest zwei im wesentlichen spiralförmig gestaltete Flügel (32, 32a und 52, 52a) aufweist, wobei jeder dieser Flügel ein vorderes, führendes Ende (34, 34a) und ein rückwärtiges Ende aufweist, wobei jedes rückwärtige Ende in axialer Richtung durch einen Winkel (α) beabstandet ist, und zwar in bezug auf die Richtung der Drehbewegung, wobei dieses Mischverfahren die folgenden Schritte aufweist:
   ausschließlicher Antrieb dieser Rotoren mit gleicher Geschwindigkeit in unterschiedlichen Richtungen auf parallelen horizontalen Achsen (30, 30a),
   Orientierung dieser Rotoren mit einer vorbestimmten Ausrichtung in Drehrichtung zueinander,
   wobei diese vorbestimmte Ausrichtung in Drehrichtung innerhalb von ± 20° einer Null-Grad-Ausrichtung der vorderen Enden der ersten Rotorflügel liegt,
   Lokalisieren eines ersten dieser Rotorflügel an jedem Rotor, um als erstes Paar von gegenüberliegenden Rotorflügeln (32, 32a) zu dienen,
   Bewegen dieses ersten Paares von einander gegenüberliegenden Rotorflügeln mit identischer Rotorgeschwindigkeit durch ein horizontales Bezugsviereck, welches durch diese Rotorachsen und diese beiden Endwände gebildet ist, wobei sich dieses erste Paar von einander gegenüberliegenden Rotorflügeln durch dieses Rechteck auf gegenüberliegenden Seiten einer ersten Diagonale (42) dieses Rechtecks beweg, wobei das vordere Ende dieses ersten Paares von einander gegenüberliegenden Rotorflügeln in der Nähe zu den jeweiligen Endwänden liegt und die Bewegung durch dieses Rechteck im wesentlichen innerhalb der gleichen ersten Zeit erfolg, um die Mischungsbestandteile zwischen diesem ersten Paar von einander gegenüberliegenden Rotorflügeln quer und axial zu quetschen,
   wobei dieses quer und axial verlaufende Quetschmischen zwischen diesem ersten Paar von einander gegenüberliegenden Rotorflügeln gegen diese erste Diagonale von entgegengesetzten Seiten dieser ersten Diagonale gerichtet ist,
   Lokalisieren von zweiten Rotorflügeln (52, 52a) auf jedem Rotor, um als zweites Paar von einander gegenüberliegenden Rotorflügeln zu dienen, wobei dieses erste und dieses zweite Paar von Rotorflügeln ihre entsprechenden vorderen Enden in gestaffelter Winkelanordnung zueinander orientiert haben, und wobei dieses zweite Paar voneinander gegenüberliegenden Rotorflügeln sich durch dieses Viereck auf entgegengesetzten Seiten einer zweiten Diagonale (44) dieses Rechtecks bewegt, wobei diese vorderen, führenden Enden dieses zweiten Paares von einander gegenüberliegenden Rotorflügeln entsprechend den Endwänden benachbart sind und sich durch das Rechteck im wesentlichen in der gleichen zweiten Zeit bewegen,
   wobei diese zweite Zeit an einem Zeitpunkt liegt, nachdem dieses erste Paar von einander gegenüberliegenden Rotorflügeln dieses Rechteck für das querlaufende und axiale Quetschmischen der Bestandteile zwischen diesem zweiten Paar voneinander gegenüberliegenden Rotorflügeln durchlaufen hat, welche sich durch dieses Rechteck bewegen, und wobei dieses quer und axial verlaufende Quetschmischen zwischen diesem zweiten Paar von einander gegenüberliegenden Rotorflügeln auf diese zweite Diagonale von einander gegenüberliegenden Seiten dieser zweiten Diagonale hin gerichtet ist, wodurch dieses quer und axial verlaufende Quetschmischen von entgegengesetzten Seiten der ersten Diagonale und von entgegengesetzten Seiten der zweiten Diagonale jeweils während jeder Umdrehung der beiden Rotoren wiederholt wird.

2. Verfahren zum Mischen gemäß Anspruch 1, welches weiterhin die folgenden Schritte aufweist:
   Lokalisieren eines dritten und eines vierten spiralförmig gestalteten Flügels auf jeden Rotor, wobei jeder Flügel ein vorderes, führendes und ein hinteres Ende aufweist, und wobei dieser dritte Flügel an jedem Rotor entgegengesetzt dem ersten Flügel dieses Rotors angebracht ist, und wobei der vierte Flügel auf jedem Rotor entgegengesetzt des zweiten Flügels auf dem Rotor angebracht ist, und
   wobei diese dritten Flügel auf dem Rotor als ein drittes Paar (62, 62a) von einander gegenüberliegenden Rotorflügeln dient, welche sich durch das Rechteck mit identischer Rotorgeschwindigkeit auf einander gegenüberliegenden Seiten dieser ersten Diagonale bewegt, wobei ihre führenden vorderen Enden den Endwänden benachbart sind und wobei die Bewegungen durch dieses Rechteck bei näherungsweise einer gleichen dritten Zeit stattfinden, wenn jeder dieser Rotoren um 180° von seiner entsprechenden Position von dieser ersten Zeit aus gedreht hat, um ein quer und axial verlaufendes Quetschmischen zwischen den Bestandteilen zwischen diesem dritten Paar von einander gegenüberliegenden Seiten dieser ersten Diagonale zu bewirken,
   wobei dieses quer und axial verlaufende Quetschmischen zwischen diesem dritten Paar von einander gegenüberliegenden Rotorflügeln zu dieser ersten Diagonale von entgegengesetzten Seiten dieser ersten Diagonale hin gerichtet ist, und
   wobei diese vierten Flügel auf dem Rotor als viertes Paar von einander gegenüberliegenden Rotorflügeln dienen, die sich durch das Rechteck mit identischer Rotorgeschwindigkeit auf einander entgegengesetzten Seiten dieser zweiten Diagonale bewegen, wobei ihre führenden Enden entsprechend benachbart zu den Endwänden sind und sich durch dieses Rechteck in näherungsweise einer vierten Zeit bewegen, um die Bestandteile zwischen diesem vierten Paar von einander gegenüberliegenden Rotorflügeln, die sich durch dieses Rechteck aufeinander gegenüberliegenden Seiten dieser zweiten Diagonale bewegen, mit einem quer- und axialverlaufenden Quetschmischen zu mischen, und
   wobei dieses quer- und axialverlaufende Quetschmischen von diesem vierten Paar von einander gegenüberliegenden Rotorflügeln zu dieser zweiten Diagonale von einander gegenüberliegenden Seiten dieser zweiten Diagonale ausgerichtet ist, und
   wobei dieses quer- und axialverlaufende Quetschmischen von entgegengesetzten Seiten dieser ersten Diagonale und von entgegengesetzten Seiten dieser zweiten Diagonale jeweils zweimal während jeder Umdrehung dieser beiden Rotoren wiederholt wird.

3. Verfahren gemäß Anspruch 1, wobei dieses erste Paar von einander gegenüberliegenden Rotorflügeln (32, 32a) eine derartige Länge in axialer Richtung aufweist, daß diese Flügel von diesem ersten Paar einander axial überlappen.

4. Verfahren gemäß Anspruch 1, wobei dieses zweite Paar von einander gegenüberliegenden Flügeln (52, 52a) eine axiale Länge aufweist, die kürzer ist, als die dieses ersten Paares von einander gegenüberliegenden Rotorflügeln.

5. Verfahren gemäß Anspruch 1, wobei dieser Winkel (α) zwischen den vorderen, führenden und hinteren Enden dieser Flügel dieses ersten Paares zumindest 90° beträgt.

6. Verfahren gemäß Anspruch 2, wobei diese zweite und vierte Paare von einander gegenüberstehenden Rotorflügeln ihre entsprechenden vorderen, führenden Enden in diametral entgegengesetzter Beziehung zueinander ausgerichtet haben, und wobei diese erste und diese dritte Paare von einander gegenüberliegenden Rotorflügeln ihre entsprechenden vorderen, führenden Enden in diametral gegenüberliegender Beziehung zueinander angeordnet haben, wobei die diametral gegenüberliegende Orientierung dieser gepaarten vorderen, führenden Enden rechtwinklig zueinander angeordnet ist.

Revendications

1. Procédé de mélange d'un lot d'ingrédients dans une mélangeuse de type à traitement par lot, présentant un carter, définissant deux cavités partiellement cylindriques, opposées horizontalement, avec des faces ouvertes placées l'une en face de l'autre et définissant une chambre (17), ledit carter comportant des ouvertures d'entrée et de sortie (11,14), espacées verticalement, communiquant avec ladite chambre et avec lesdites cavités, des parois d'extrémité (36,38) opposées axialement, pour lesdites cavités et chambre, un coulisseau (10), pour obturer ladite ouverture d'entrée, une porte (14) pour obturer ladite ouverture de sortie,
deux rotors de mélange (13,13a), opposés et non-engrenés l'un dans l'autre, chacun desdits rotors étant prévu dans une cavité respective, chaque rotor présentant au moins deux ailettes (32,32a,52,52a), en forme générale hélicoïdale, chaque ailette présentant une extrémité avant (34,34a) et une extrémité arrière, chaque extrémité arrière étant espacée circonférentiellement à l'arrière de son extrémité avant de la valeur d'un angle (α) par rapport au sens de direction du rotor, ledit procédé de mélange comprenant les étapes consistant à :
   entraîner lesdits rotors seulement à une vitesse égale dans des sens opposés sur des axes horizontaux parallèles (30,30a),
   orienter lesdits rotors l'un par rapport à l'autre suivant une relation de positionnement en rotation prédéterminée,
   ledit positionnement en rotation prédéterminé étant situé dans la plage de ± 20° par rapport à l'alignement à 0° des extrémités avant des premières ailettes de rotor,
   placer une première desdites ailettes de rotor, sur chaque rotor, pour servir de premier couple d'ailettes de rotor opposées (32,32a), déplacer ledit premier couple d'ailettes de rotor opposées à une vitesse de rotor égale, en passant dans un rectangle de référence horizontal, défini par lesdits axes de rotor et lesdites deux parois d'extrémité, ledit premier couple d'ailettes de rotor opposées se déplaçant dans ledit rectangle, sur des côtés opposés par rapport à une première diagonale (42) dudit rectangle, avec lesdites extrémités avant de ladite première paire d'ailettes de rotor opposées adjacentes respectivement aux parois d'extrémité et se déplaçant dans ledit rectangle, sensiblement au même moment, pour produire un mélange avec malaxage transversal et axial des ingrédients, entre ledit premier couple d'ailettes de rotor opposées,
   ledit mélange à malaxage transversal et axial entre ledit premier couple d'ailettes de rotor opposées étant effectué en direction de ladite première diagonale, par rapport aux côtés opposés de ladite première diagonale, placer une seconde desdites ailettes de rotor (52,52a) sur chaque rotor, pour servir de second couple d'ailettes de rotor opposées, lesdits premier et second couple d'ailettes de rotor présentant leurs extrémités avant respectives en position angulaire en quinconce par rapport à la machine, ladite seconde paire d'ailettes de rotor opposées passant dans ledit rectangle sur les côtés opposés d'une seconde diagonale (44) dudit rectangle, avec lesdites extrémités avant dudit second couple d'ailettes de rotor opposées adjacentes respectivement aux parois d'extrémité et se déplaçant dans ledit rectangle sensiblement au même moment,
   ledit second moment étant situé à un moment ultérieur au moment où le premier couple d'ailettes de rotor opposées sont passées dans ledit rectangle, pour mélanger avec malaxage transversal et axial les ingrédients, entre ledit second couple d'ailettes de rotor opposées, en se déplaçant dans ledit rectangle, et
   ledit mélange avec malaxage transversal et axial, entre ledit second couple d'ailettes de rotor opposées s'effectuant vers ladite seconde diagonale, en partant des côtés opposés de ladite seconde diagonale,
   de manière que ledit mélange à malaxage transversal et axial partant des côtés opposés de ladite première diagonale et des côtés opposés de ladite seconde diagonale soit chaque fois répété à chaque rotation des deux rotors.

2. Procédé selon la revendication 1, comprenant en outres les étapes consistant à :
   placer une troisième ailette de forme hélicoïdale sur chaque rotor, chaque ailette présentant une extrémité avant et une extrémité arrière, avec ladite troisième ailette sur chaque rotor, placée à l'opposé de la première ailette sur le rotor et avec la quatrième ailette sur chaque rotor placée à l'opposé de la seconde ailette sur le rotor,
   lesdites troisièmes ailettes des rotors, servant de troisième couple (62,62a) d'ailettes de rotor opposées, passant dans le rectangle à une vitesse de rotor égale et sur les côtés opposés de ladite première diagonale, avec leurs extrémités avant adjacentes respectivement aux parois d'extrémité et se déplaçant dans ledit rectangle à approximativement une troisième fois lorsque chacun desdits rotor a tourné de 180° par rapport à sa position respective audit premier moment, pour produire un mélange à malaxage transversal et axial des ingrédients, entre ledit troisième couple de côtés opposés de ladite première diagonale,
   ledit mélange à malaxage transversal et axial entre ledit troisième couple d'ailettes de rotor opposées s'effectuant en direction de ladite première diagonale, en partant des côtés opposés de ladite première diagonale,
   lesdites quatrième ailettes des rotors, servant de quatrième paire d'ailette de rotor opposées, passant dans le rectangle à une vitesse égale à celle du rotor, sur les côtés opposés de ladite seconde diagonale, avec leurs extrémités avant adjacentes respectivement aux parois d'extrémité et se déplaçant dans ledit rectangle à peu près une quatrième fois, pour produire un mélange à malaxage axial et transversal, entre ledit quatrième couple d'ailettes de rotor opposées qui se déplace dans ledit rectangle, sur les côtés opposés de ladite seconde diagonale,
   ledit mélange avec malaxage transversal et axial, entre ledit quatrième couple d'ailettes de rotor opposées s'effectuant vers ladite seconde diagonale, en partant des côtés opposés de ladite seconde diagonale,
   de manière que ledit mélange à malaxage transversal et axial partant des côtés opposés de ladite première diagonale et des côtés opposés de ladite seconde diagonale soit chaque fois répété deux fois à chaque rotation des deux rotors.

3. Procédé selon la revendication 1, dans lequel ledit premier couple d'ailettes de rotor opposées (32,32a) présente une longueur suffisante en direction axiale, de telle façon que lesdites ailettes dudit premier couple se chevauchent les unes les autres axialement.

4. Procédé selon la revendication 1, dans lequel ledit second couple d'ailettes de rotor opposées (52,52a) présente une longueur axiale plus courte que celle dudit premier couple d'ailettes de rotor opposées.

5. Procédé selon la revendication 1, dans lequel ledit angle (α) entre les extrémités avant et arrière de chacune desdites ailettes dudit premier couple est d'au moins 90 degrés.

6. Procédé selon la revendication 2, dans lequel lesdits second et quatrième couples d'ailettes de rotor opposées présentent leurs extrémités avant respectives orientées mutuellement en une relation diamétralement opposée, et dans lequel lesdits premier et troisième couple d'ailettes de rotor opposées présentent leurs extrémités avant respectives orientées mutuellement en une relation diamétralement opposée, ladite orientation diamétralement opposée desdits couples d'ailettes avant étant disposée mutuellement à angle droit.

Drawing